US20100013296A1 - Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel - Google Patents
Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel Download PDFInfo
- Publication number
- US20100013296A1 US20100013296A1 US12/174,385 US17438508A US2010013296A1 US 20100013296 A1 US20100013296 A1 US 20100013296A1 US 17438508 A US17438508 A US 17438508A US 2010013296 A1 US2010013296 A1 US 2010013296A1
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- United States
- Prior art keywords
- wheel
- pressure
- brake pressure
- modulated
- wheel speed
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/44—Actuating mechanisms
- B64C25/46—Brake regulators for preventing skidding or aircraft somersaulting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
- B60T8/17—Using electrical or electronic regulation means to control braking
- B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
- B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
- B60T8/32—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration
- B60T8/88—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration with failure responsive means, i.e. means for detecting and indicating faulty operation of the speed responsive control means
- B60T8/885—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration with failure responsive means, i.e. means for detecting and indicating faulty operation of the speed responsive control means using electrical circuitry
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T2270/00—Further aspects of brake control systems not otherwise provided for
- B60T2270/40—Failsafe aspects of brake control systems
- B60T2270/402—Back-up
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T2270/00—Further aspects of brake control systems not otherwise provided for
- B60T2270/40—Failsafe aspects of brake control systems
- B60T2270/416—Wheel speed sensor failure
Definitions
- This invention relates generally to aircraft braking systems, and more particularly concerns a method for maintaining optimal braking and skid protection for a two-wheeled vehicle wheel with a wheel speed sensor failure.
- the present invention provides for a method for controlling antiskid braking of a vehicle such as an aircraft having a plurality of wheels with a wheel speed sensor for each wheel, when a wheel speed sensor of one of the wheels fails, by providing pulsed braking pressure to the affected wheel, and determining the braking pressure to be pulsed to the affected wheel, based upon whether an incipient or initial skid on another wheel not affected by a wheel speed sensor failure has been detected.
- the method of the invention allows safe braking to continue in an antiskid braking system that can otherwise result in asymmetric braking, or proportional braking without antiskid protection that could lead to tire failure, both of which are particularly significant for an aircraft having only two braked wheels.
- the method of the invention allows antiskid braking on a wheel with a failed sensor to be maintained, which improves stopping performance and safety margins.
- the present invention accordingly provides for a method for controlling antiskid braking of an aircraft having two or more wheels in a group of wheels, such as a pair of wheels, for example, with a wheel speed sensor associated with each wheel for antiskid control of the group of wheels.
- a wheel speed sensor associated with each wheel for antiskid control of the group of wheels.
- the commanded braking pressure of the second wheel is used as a brake pressure limit of the first wheel.
- a maximum brake pressure of the first wheel is then determined to be a first desired fraction of the brake pressure limit of the first wheel.
- a modulated brake pressure is then determined as a second desired fraction of the maximum brake pressure of the first wheel, and modulated pressure pulses of the modulated brake pressure are provided to the first wheel.
- the maximum brake pressure of the first wheel is determined to be the highest commanded braking pressure of the second wheel.
- a commanded braking pressure of the first wheel is monitored, and the modulated brake pressure to the first wheel is limited to be less than the commanded braking pressure of the first wheel.
- the modulated brake pressure to the first wheel may be limited to be a third desired fraction of the commanded braking pressure of the first wheel.
- the modulated pressure pulses are modulated to have a constant period and duty cycle between a return pressure and the modulated pulsed pressure.
- the FIGURE is a schematic flow diagram illustrating the steps of the method of the invention.
- the present invention provides for an antiskid system and method for maintaining optimal braking and skid protection for a vehicle, such as a two-wheeled vehicle, such as an aircraft, for example, containing redundant hydraulic systems with split cavity brake pistons.
- the method of the invention becomes operative in the event of a loss of wheel speed sensing on a wheel, if there is a functioning wheel speed sensor on another wheel.
- braking pressure to the affected wheel is modulated with a constant period and duty cycle between return pressure and a calculated maximum pulsed pressure, to allow the brake control system to maintain optimal braking on the affected wheel.
- the pulsed brake pressure is limited to the brake command that caused the last incipient or initial skid on the other wheel, scaled by a factor for safety. Every time the brake control system detects the start of an incipient or initial skid on the wheel with the functioning speed sensor, that brake pressure scaled by a factor is set as the maximum brake pressure on the pulsed wheel.
- the pulsed pressure on the wheel with the failed speed sensor is limited to be no greater than the greatest brake pressure that has been commanded on the wheel with the functioning wheel speed sensor. This prevents the affected wheel from skidding, and enables the pilot to achieve directional control with differential braking.
- the maximum pulsed pressure for the wheel with the failed wheel sensor may also be limited to be less than the brake pressure command from the pilot's input at the brake pedals, allowing directional control to be maintained during a landing.
- the pressure can be applied and reduced instantly, or ramped to prevent causing a skid due to pressure overshoots.
- each wheel has its own wheel speed sensor, such as a pair of wheels A and B, for example, once it is determined that there is a complete loss of wheel speed sensing on one of the wheels, such as wheel A, for example, and if there is a functioning wheel speed sensor on another wheel of the group, such as wheel B, the method of the invention illustrated in the FIGURE is activated.
- the maximum brake pressure on the wheel A to be pulsed, P MAX A is typically initialized 10 to a value such as zero, for example.
- the commanded braking pressure P COM B of the other wheel B is measured at 12 , and if an incipient or initial skid on wheel B has been detected, based upon wheel speed signals from the associated wheel speed sensor, the commanded brake pressure P COM B that caused the last incipient or initial skid on the wheel B is stored at 14 as the LAST P SKID B , and this value is used as a limit of the brake pressure on the wheel A to be pulsed.
- the commanded brake pressure P COM B is compared at 18 with the maximum brake pressure on the wheel A to be pulsed, P MAX A , and the highest commanded brake pressure P COM B is stored as the maximum brake pressure on the wheel A to be pulsed, P MAX A , at 20 .
- the pulsed pressure P PULSE A on the wheel A with the failed speed sensor will be limited at 22 to be to a percentage value, such as 95-100%, for example, of the maximum brake pressure on the wheel A to be pulsed, P MAX A , so as to be no greater than the greatest commanded brake pressure P COM B on the healthy wheel, for the duration of the landing. This prevents the pulsed wheel from skidding and maintains the ability of the pilot to achieve directional control with differential braking.
- the brake pressure command from the pilot's input at the brake pedals P COM A is also measured at 24 , and the maximum pulsed pressure P PULSE A on the wheel A for the failed channel is compared at 26 with the commanded brake pressure P COM A , and limited at 28 to be less than the commanded brake pressure P COM A , such as 95-100%, for example, of the commanded brake pressure P COM A .
- the brake pressure command for the wheel with the failed sensor will provide a modulated pressure pulse, PULSE A, at 30 , with a constant period and duty cycle between return pressure and a calculated maximum pulsed pressure, P PULSE A , on the wheel A with the failed wheel speed sensor.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Regulating Braking Force (AREA)
- Valves And Accessory Devices For Braking Systems (AREA)
Abstract
Description
- This invention relates generally to aircraft braking systems, and more particularly concerns a method for maintaining optimal braking and skid protection for a two-wheeled vehicle wheel with a wheel speed sensor failure.
- Automatic braking systems commonly have been provided on commercial, military, and large turbine aircraft to aid the deceleration of the aircraft upon landing. Modern aircraft braking systems typically optimize braking efficiency by adapting to runway conditions and other factors affecting braking to maximize deceleration, corresponding to the level of brake pressure selected by the pilot. Antiskid systems for military, small business jets and general aviation airplanes have traditionally utilized antiskid control systems that sense wheel speed from left and right wheel speed sensors.
- Individual wheel antiskid control systems typically use separate control channels for each wheel and individual wheel antiskid valves. Peak efficiency is maintained on both wheels, so that the shortest stopping distance is achieved. However, in the event of a failed wheel speed sensor, there exists the possibility that brake pressure reduction on one wheel due to antiskid activity will cause a shift in airplane direction during a temporary brake pressure imbalance.
- There were previously two options in the event of a failed wheel speed sensor. One option was to inhibit braking on that wheel. This is not practical on some aircraft, especially with only two braked wheels, because of the loss of directional control and the increase in stopping distance. The second option was to pulse the brake pressure on and off up to the brake pressure command from the pilot's brake pedals. This method prevents blown tires and allows directional control, but causes significant loads on the landing gear structure due to the occurrence of periodic skid events caused by brake pressure application. These loads can be high enough to cause excessive wear and possibly failure of the landing gear.
- It would be desirable to provide pulsed brake pressure to a wheel with a speed sensor failure, to periodically release brake pressure on the wheel, allowing the wheel to spin up, in order to protect against tire failure due to lockup. Particularly for a two-wheeled vehicle with a wheel affected by a speed sensor failure, it would also be desirable to apply a fraction of the skid pressure from another wheel with a functioning wheel speed sensor to the affected wheel to prevent the brake pressure on the affected wheel from being large enough to skid, in most conditions. It would also not be desirable to inhibit braking on a wheel with a failed speed sensor, because maintaining braking on the affected wheel allows the pilot to maintain directional control using differential braking. For a two-wheeled vehicle with a wheel affected by a wheel speed sensor failure, it would also be desirable to limit the brake pressure on the affected wheel to a value below the skid brake pressure on the opposite wheel, in order to greatly improve stability margins on the landing gear. The present invention meets these and other needs.
- Briefly, and in general terms, the present invention provides for a method for controlling antiskid braking of a vehicle such as an aircraft having a plurality of wheels with a wheel speed sensor for each wheel, when a wheel speed sensor of one of the wheels fails, by providing pulsed braking pressure to the affected wheel, and determining the braking pressure to be pulsed to the affected wheel, based upon whether an incipient or initial skid on another wheel not affected by a wheel speed sensor failure has been detected. The method of the invention allows safe braking to continue in an antiskid braking system that can otherwise result in asymmetric braking, or proportional braking without antiskid protection that could lead to tire failure, both of which are particularly significant for an aircraft having only two braked wheels. The method of the invention allows antiskid braking on a wheel with a failed sensor to be maintained, which improves stopping performance and safety margins.
- The present invention accordingly provides for a method for controlling antiskid braking of an aircraft having two or more wheels in a group of wheels, such as a pair of wheels, for example, with a wheel speed sensor associated with each wheel for antiskid control of the group of wheels. In one aspect of the method of the invention, if a first wheel speed sensor of a first wheel has failed, and a second wheel speed sensor of a second wheel is functioning, if an incipient or initial skid of the second wheel associated with a commanded braking pressure of the second wheel has occurred, the commanded braking pressure of the second wheel is used as a brake pressure limit of the first wheel. A maximum brake pressure of the first wheel is then determined to be a first desired fraction of the brake pressure limit of the first wheel. A modulated brake pressure is then determined as a second desired fraction of the maximum brake pressure of the first wheel, and modulated pressure pulses of the modulated brake pressure are provided to the first wheel.
- In another aspect of the method of the invention, if an incipient or initial skid of the second wheel has not occurred, the maximum brake pressure of the first wheel is determined to be the highest commanded braking pressure of the second wheel.
- In another aspect of the method of the invention, a commanded braking pressure of the first wheel is monitored, and the modulated brake pressure to the first wheel is limited to be less than the commanded braking pressure of the first wheel. The modulated brake pressure to the first wheel may be limited to be a third desired fraction of the commanded braking pressure of the first wheel. In a presently preferred aspect, the modulated pressure pulses are modulated to have a constant period and duty cycle between a return pressure and the modulated pulsed pressure.
- These and other aspects and advantages of the invention will become apparent from the following detailed description, and the accompanying drawing which illustrates, by way of example, the features of the invention.
- The FIGURE is a schematic flow diagram illustrating the steps of the method of the invention.
- Referring to the drawing, which is provided by way of example, and not by way of limitation, the present invention provides for an antiskid system and method for maintaining optimal braking and skid protection for a vehicle, such as a two-wheeled vehicle, such as an aircraft, for example, containing redundant hydraulic systems with split cavity brake pistons. The method of the invention becomes operative in the event of a loss of wheel speed sensing on a wheel, if there is a functioning wheel speed sensor on another wheel. In response to a brake pressure command for the affected wheel with the failed sensor, braking pressure to the affected wheel is modulated with a constant period and duty cycle between return pressure and a calculated maximum pulsed pressure, to allow the brake control system to maintain optimal braking on the affected wheel. The pulsed brake pressure is limited to the brake command that caused the last incipient or initial skid on the other wheel, scaled by a factor for safety. Every time the brake control system detects the start of an incipient or initial skid on the wheel with the functioning speed sensor, that brake pressure scaled by a factor is set as the maximum brake pressure on the pulsed wheel.
- If an incipient or initial skid has not been detected on the wheel with the functioning wheel speed sensor during the current landing, the pulsed pressure on the wheel with the failed speed sensor is limited to be no greater than the greatest brake pressure that has been commanded on the wheel with the functioning wheel speed sensor. This prevents the affected wheel from skidding, and enables the pilot to achieve directional control with differential braking.
- In another aspect, the maximum pulsed pressure for the wheel with the failed wheel sensor may also be limited to be less than the brake pressure command from the pilot's input at the brake pedals, allowing directional control to be maintained during a landing. The pressure can be applied and reduced instantly, or ramped to prevent causing a skid due to pressure overshoots.
- Referring to the FIGURE, for two or more wheels of a group of wheels in which each wheel has its own wheel speed sensor, such as a pair of wheels A and B, for example, once it is determined that there is a complete loss of wheel speed sensing on one of the wheels, such as wheel A, for example, and if there is a functioning wheel speed sensor on another wheel of the group, such as wheel B, the method of the invention illustrated in the FIGURE is activated. The maximum brake pressure on the wheel A to be pulsed, PMAX A, is typically initialized 10 to a value such as zero, for example. The commanded braking pressure PCOM B of the other wheel B is measured at 12, and if an incipient or initial skid on wheel B has been detected, based upon wheel speed signals from the associated wheel speed sensor, the commanded brake pressure PCOM B that caused the last incipient or initial skid on the wheel B is stored at 14 as the LAST PSKID B, and this value is used as a limit of the brake pressure on the wheel A to be pulsed. Every time the brake control system detects the start of an incipient or initial skid on the wheel B with the functioning speed sensor, that brake pressure, LAST PSKID B, scaled by a percentage factor, such as 90-99%, for example, is set as the maximum brake pressure PPULSE A on the pulsed wheel at 16.
- If wheel B with the functioning speed sensor has not yet experienced any initial or incipient skidding during the current wheel braking, such as during a landing, for example, the commanded brake pressure PCOM B is compared at 18 with the maximum brake pressure on the wheel A to be pulsed, PMAX A, and the highest commanded brake pressure PCOM B is stored as the maximum brake pressure on the wheel A to be pulsed, PMAX A, at 20. The pulsed pressure PPULSE A on the wheel A with the failed speed sensor will be limited at 22 to be to a percentage value, such as 95-100%, for example, of the maximum brake pressure on the wheel A to be pulsed, PMAX A, so as to be no greater than the greatest commanded brake pressure PCOM B on the healthy wheel, for the duration of the landing. This prevents the pulsed wheel from skidding and maintains the ability of the pilot to achieve directional control with differential braking.
- The brake pressure command from the pilot's input at the brake pedals PCOM A is also measured at 24, and the maximum pulsed pressure PPULSE A on the wheel A for the failed channel is compared at 26 with the commanded brake pressure PCOM A, and limited at 28 to be less than the commanded brake pressure PCOM A, such as 95-100%, for example, of the commanded brake pressure PCOM A. The brake pressure command for the wheel with the failed sensor will provide a modulated pressure pulse, PULSE A, at 30, with a constant period and duty cycle between return pressure and a calculated maximum pulsed pressure, PPULSE A, on the wheel A with the failed wheel speed sensor.
- It should be apparent from the foregoing that the presently described system and method is applicable to various types of vehicles. Aircraft, automobiles, trucks and trains all have the need for some type of anti-skid braking control. The present invention can readily be used on any such vehicles.
- It will also be apparent from the foregoing that while particular forms of the invention have been illustrated and described, various modifications can be made without departing from the spirit and scope of the invention. Accordingly, it is not intended that the invention be limited, except as by the appended claims.
Claims (18)
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
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US12/174,385 US8083295B2 (en) | 2008-07-16 | 2008-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
ES09790535.0T ES2524365T3 (en) | 2008-07-16 | 2009-07-16 | Method to maintain optimal braking and non-slip protection for a two-wheel vehicle that has a single-wheel speed sensor failure |
CN2009801275916A CN102099230B (en) | 2008-07-16 | 2009-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
CA2730924A CA2730924A1 (en) | 2008-07-16 | 2009-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
JP2011518912A JP5426674B2 (en) | 2008-07-16 | 2009-07-16 | How to maintain optimal braking and skid protection in a two-wheeled vehicle with a single wheel speed sensor failure |
PCT/US2009/050852 WO2010009317A1 (en) | 2008-07-16 | 2009-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
BRPI0915949A BRPI0915949B8 (en) | 2008-07-16 | 2009-07-16 | METHOD FOR CONTROLLING ANTI-SKID BRAKING OF A PLURALITY OF WHEELS IN AN AIRCRAFT WHEEL GROUP AND METHOD FOR CONTROLLING ANTI-SKID BRAKING OF FIRST AND SECOND PAIRED WHEELS OF AN AIRCRAFT |
EP09790535.0A EP2318243B1 (en) | 2008-07-16 | 2009-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,195 US8326506B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,234 US8346454B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/673,673 US9056673B2 (en) | 2008-07-16 | 2012-11-09 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/174,385 US8083295B2 (en) | 2008-07-16 | 2008-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
Related Child Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/227,234 Division US8346454B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,195 Division US8326506B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
Publications (2)
Publication Number | Publication Date |
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US20100013296A1 true US20100013296A1 (en) | 2010-01-21 |
US8083295B2 US8083295B2 (en) | 2011-12-27 |
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Application Number | Title | Priority Date | Filing Date |
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US12/174,385 Active 2030-10-07 US8083295B2 (en) | 2008-07-16 | 2008-07-16 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,195 Active US8326506B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,234 Active US8346454B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/673,673 Active 2029-05-17 US9056673B2 (en) | 2008-07-16 | 2012-11-09 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
Family Applications After (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/227,195 Active US8326506B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/227,234 Active US8346454B2 (en) | 2008-07-16 | 2011-09-07 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US13/673,673 Active 2029-05-17 US9056673B2 (en) | 2008-07-16 | 2012-11-09 | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
Country Status (8)
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US (4) | US8083295B2 (en) |
EP (1) | EP2318243B1 (en) |
JP (1) | JP5426674B2 (en) |
CN (1) | CN102099230B (en) |
BR (1) | BRPI0915949B8 (en) |
CA (1) | CA2730924A1 (en) |
ES (1) | ES2524365T3 (en) |
WO (1) | WO2010009317A1 (en) |
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EP3115267A1 (en) * | 2015-07-08 | 2017-01-11 | Airbus Operations Limited | Data processing unit for aircraft undercarriage performance monitoring |
EP3115266A1 (en) * | 2015-07-08 | 2017-01-11 | Airbus Operations Limited | Braking control system for an aircraft |
US20170173374A1 (en) * | 2012-08-10 | 2017-06-22 | The Reliable Automatic Sprinkler Co., Inc. | In-rack fire protection sprinkler system |
EP3530565A1 (en) * | 2018-02-26 | 2019-08-28 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
EP3835151A1 (en) * | 2019-12-11 | 2021-06-16 | Continental Teves AG & Co. OHG | Method for controlling a brake system of a vehicle |
US11358710B2 (en) | 2018-02-23 | 2022-06-14 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
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US8083295B2 (en) | 2008-07-16 | 2011-12-27 | Hydro-Aire, Inc. | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
US8965657B2 (en) * | 2013-07-02 | 2015-02-24 | Goodrich Corporation | System and method for detecting an on ground condition of an aircraft |
CN106394881B (en) * | 2016-10-18 | 2018-08-07 | 西安航空制动科技有限公司 | A kind of Aircraft Anti-skid Break Control power-on self-test guard method |
US10472054B2 (en) | 2017-02-21 | 2019-11-12 | Goodrich Corporation | Antiskid operation during degraded operation |
CN112623200B (en) * | 2020-12-29 | 2022-11-22 | 中国航空工业集团公司西安飞机设计研究所 | Brake control method for airplane skid resistance failure |
Citations (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3711163A (en) * | 1970-09-30 | 1973-01-16 | Goodyear Tire & Rubber | Automatic braking system |
US3768873A (en) * | 1971-06-23 | 1973-10-30 | Crane Co | Brake control system |
US3856365A (en) * | 1972-10-03 | 1974-12-24 | Goodyear Tire & Rubber | Anti-skid control system for aircraft |
US3880475A (en) * | 1972-03-29 | 1975-04-29 | Goodyear Tire & Rubber | Anti-skid system |
US4005911A (en) * | 1975-10-06 | 1977-02-01 | Wabco Westinghouse Gmbh | Individual wheel antiskid brake control system arranged to prevent excessive brake pressure differences |
US4007970A (en) * | 1975-09-30 | 1977-02-15 | The Boeing Company | Aircraft automatic braking system |
US4078845A (en) * | 1976-08-13 | 1978-03-14 | The Boeing Company | Limited-slip brake control system |
US4120540A (en) * | 1973-09-06 | 1978-10-17 | The Boeing Company | Aircraft automatic braking system |
US4130322A (en) * | 1976-11-16 | 1978-12-19 | Crane Co. | Single gain skid control valve and skid control system |
US4231442A (en) * | 1974-06-15 | 1980-11-04 | Mogens Birkeholm | Apparatus for braking a train of vehicles |
US4269455A (en) * | 1978-08-14 | 1981-05-26 | Goodyear Aerospace Corporation | Antiskid brake control system |
US4404633A (en) * | 1980-01-11 | 1983-09-13 | Societe Nationale Industrielle Aerospatiale | Process and device for braking an aircraft by seeking an optimal sliding of the braked wheels |
US4412291A (en) * | 1980-09-30 | 1983-10-25 | The Boeing Company | Brake torque control system |
US4986610A (en) * | 1989-02-21 | 1991-01-22 | Aircraft Braking Systems Corporation | Brake system with brake selection means |
US5019774A (en) * | 1988-08-05 | 1991-05-28 | The Boeing Company | Method and apparatus for sensing the rotational speed of an aircraft wheel with an amplifier and transducer located in the wheel and a circuit to check the integrity of the transducer |
US5024491A (en) * | 1976-11-18 | 1991-06-18 | The Boeing Company | Automatic aircraft braking system including wheelspeed responsive control apparatus |
US5172960A (en) * | 1991-02-12 | 1992-12-22 | Aerospatiale Societe Nationale Industrielle | Brake control minimizing the number of brakes activated and optimizing wear conditions |
US5397173A (en) * | 1993-03-08 | 1995-03-14 | Messier-Bugatti | Electro-hydraulic braking system for the wheels of an aircraft |
US5417477A (en) * | 1993-02-01 | 1995-05-23 | Messier-Bugatti | Method of controlling an electrohydraulic braking apparatus for an aircraft wheel set, and an apparatus for implementing said method |
US5511863A (en) * | 1992-10-26 | 1996-04-30 | Alliedsignal Inc. | Hybrid brake control system |
US5707118A (en) * | 1995-09-15 | 1998-01-13 | Alliedsignal, Inc. | Velocity based brake control system with directional stability |
US5845975A (en) * | 1993-03-06 | 1998-12-08 | Dunlop Limited | Sequential selective operation of aircraft brakes |
US5918951A (en) * | 1997-05-09 | 1999-07-06 | The B.F. Goodrich Company | Antiskid brake control system using kalman filtering |
US6517171B2 (en) * | 1999-11-30 | 2003-02-11 | Nisshinbo Industries, Inc | Braking force distribution control for a four wheel drive vehicle |
US20050040286A1 (en) * | 2003-08-14 | 2005-02-24 | Radford Michael A. | Methods and systems for controlling wheel brakes on aircraft and other vehicles |
US20090276133A1 (en) * | 2008-05-05 | 2009-11-05 | Goodrich Corporation | Aircraft brake control system and method |
US20100117447A1 (en) * | 2007-05-21 | 2010-05-13 | Goodrich Corporation | Fault tolerant aircraft braking control using alternate wheel speed information |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2742978B2 (en) * | 1993-11-04 | 1998-04-22 | 住友精密工業株式会社 | Anti-skid device |
DE19511161A1 (en) * | 1995-03-27 | 1996-10-02 | Bosch Gmbh Robert | Brake system for a motor vehicle |
US6132016A (en) * | 1997-05-02 | 2000-10-17 | Hydro-Aire, Inc. | System and method for adaptive brake application and initial skid detection |
US6722745B2 (en) * | 1997-05-02 | 2004-04-20 | Hydro-Aire, Inc. | System and method for adaptive brake application and initial skid detection |
JP2000335395A (en) * | 1999-05-25 | 2000-12-05 | Unisia Jecs Corp | Brake control device |
US8083295B2 (en) | 2008-07-16 | 2011-12-27 | Hydro-Aire, Inc. | Method of maintaining optimal braking and skid protection for a two-wheeled vehicle having a speed sensor failure on a single wheel |
-
2008
- 2008-07-16 US US12/174,385 patent/US8083295B2/en active Active
-
2009
- 2009-07-16 JP JP2011518912A patent/JP5426674B2/en active Active
- 2009-07-16 ES ES09790535.0T patent/ES2524365T3/en active Active
- 2009-07-16 CA CA2730924A patent/CA2730924A1/en not_active Abandoned
- 2009-07-16 BR BRPI0915949A patent/BRPI0915949B8/en active IP Right Grant
- 2009-07-16 EP EP09790535.0A patent/EP2318243B1/en active Active
- 2009-07-16 CN CN2009801275916A patent/CN102099230B/en active Active
- 2009-07-16 WO PCT/US2009/050852 patent/WO2010009317A1/en active Application Filing
-
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- 2011-09-07 US US13/227,195 patent/US8326506B2/en active Active
- 2011-09-07 US US13/227,234 patent/US8346454B2/en active Active
-
2012
- 2012-11-09 US US13/673,673 patent/US9056673B2/en active Active
Patent Citations (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3711163A (en) * | 1970-09-30 | 1973-01-16 | Goodyear Tire & Rubber | Automatic braking system |
US3768873A (en) * | 1971-06-23 | 1973-10-30 | Crane Co | Brake control system |
US3880475A (en) * | 1972-03-29 | 1975-04-29 | Goodyear Tire & Rubber | Anti-skid system |
US3856365A (en) * | 1972-10-03 | 1974-12-24 | Goodyear Tire & Rubber | Anti-skid control system for aircraft |
US4120540A (en) * | 1973-09-06 | 1978-10-17 | The Boeing Company | Aircraft automatic braking system |
US4231442A (en) * | 1974-06-15 | 1980-11-04 | Mogens Birkeholm | Apparatus for braking a train of vehicles |
US4007970A (en) * | 1975-09-30 | 1977-02-15 | The Boeing Company | Aircraft automatic braking system |
US4005911A (en) * | 1975-10-06 | 1977-02-01 | Wabco Westinghouse Gmbh | Individual wheel antiskid brake control system arranged to prevent excessive brake pressure differences |
US4078845A (en) * | 1976-08-13 | 1978-03-14 | The Boeing Company | Limited-slip brake control system |
US4130322A (en) * | 1976-11-16 | 1978-12-19 | Crane Co. | Single gain skid control valve and skid control system |
US5024491A (en) * | 1976-11-18 | 1991-06-18 | The Boeing Company | Automatic aircraft braking system including wheelspeed responsive control apparatus |
US4269455A (en) * | 1978-08-14 | 1981-05-26 | Goodyear Aerospace Corporation | Antiskid brake control system |
US4404633A (en) * | 1980-01-11 | 1983-09-13 | Societe Nationale Industrielle Aerospatiale | Process and device for braking an aircraft by seeking an optimal sliding of the braked wheels |
US4412291A (en) * | 1980-09-30 | 1983-10-25 | The Boeing Company | Brake torque control system |
US5019774A (en) * | 1988-08-05 | 1991-05-28 | The Boeing Company | Method and apparatus for sensing the rotational speed of an aircraft wheel with an amplifier and transducer located in the wheel and a circuit to check the integrity of the transducer |
US4986610A (en) * | 1989-02-21 | 1991-01-22 | Aircraft Braking Systems Corporation | Brake system with brake selection means |
US5172960A (en) * | 1991-02-12 | 1992-12-22 | Aerospatiale Societe Nationale Industrielle | Brake control minimizing the number of brakes activated and optimizing wear conditions |
US5511863A (en) * | 1992-10-26 | 1996-04-30 | Alliedsignal Inc. | Hybrid brake control system |
US5417477A (en) * | 1993-02-01 | 1995-05-23 | Messier-Bugatti | Method of controlling an electrohydraulic braking apparatus for an aircraft wheel set, and an apparatus for implementing said method |
US5845975A (en) * | 1993-03-06 | 1998-12-08 | Dunlop Limited | Sequential selective operation of aircraft brakes |
US5397173A (en) * | 1993-03-08 | 1995-03-14 | Messier-Bugatti | Electro-hydraulic braking system for the wheels of an aircraft |
US5707118A (en) * | 1995-09-15 | 1998-01-13 | Alliedsignal, Inc. | Velocity based brake control system with directional stability |
US5918951A (en) * | 1997-05-09 | 1999-07-06 | The B.F. Goodrich Company | Antiskid brake control system using kalman filtering |
US6517171B2 (en) * | 1999-11-30 | 2003-02-11 | Nisshinbo Industries, Inc | Braking force distribution control for a four wheel drive vehicle |
US20050040286A1 (en) * | 2003-08-14 | 2005-02-24 | Radford Michael A. | Methods and systems for controlling wheel brakes on aircraft and other vehicles |
US20100117447A1 (en) * | 2007-05-21 | 2010-05-13 | Goodrich Corporation | Fault tolerant aircraft braking control using alternate wheel speed information |
US20090276133A1 (en) * | 2008-05-05 | 2009-11-05 | Goodrich Corporation | Aircraft brake control system and method |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170173374A1 (en) * | 2012-08-10 | 2017-06-22 | The Reliable Automatic Sprinkler Co., Inc. | In-rack fire protection sprinkler system |
EP3115267A1 (en) * | 2015-07-08 | 2017-01-11 | Airbus Operations Limited | Data processing unit for aircraft undercarriage performance monitoring |
EP3115266A1 (en) * | 2015-07-08 | 2017-01-11 | Airbus Operations Limited | Braking control system for an aircraft |
US9892571B2 (en) | 2015-07-08 | 2018-02-13 | Airbus Operations Limited | Data processing unit for aircraft undercarriage performance monitoring |
US10081346B2 (en) | 2015-07-08 | 2018-09-25 | Airbus Operations Limited | Braking control system for an aircraft |
CN111483589A (en) * | 2015-07-08 | 2020-08-04 | 空中客车英国运营有限责任公司 | Brake control system for aircraft |
US11358710B2 (en) | 2018-02-23 | 2022-06-14 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
EP3530565A1 (en) * | 2018-02-26 | 2019-08-28 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
US20190263506A1 (en) * | 2018-02-26 | 2019-08-29 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
US10933982B2 (en) * | 2018-02-26 | 2021-03-02 | The Boeing Company | Methods and apparatus for controlling landing gear retract braking |
EP3835151A1 (en) * | 2019-12-11 | 2021-06-16 | Continental Teves AG & Co. OHG | Method for controlling a brake system of a vehicle |
US20210179045A1 (en) * | 2019-12-11 | 2021-06-17 | Continental Teves Ag & Co. Ohg | Method for controlling a brake system of a vehicle |
Also Published As
Publication number | Publication date |
---|---|
JP5426674B2 (en) | 2014-02-26 |
EP2318243B1 (en) | 2014-11-12 |
CN102099230B (en) | 2013-07-10 |
US20110320100A1 (en) | 2011-12-29 |
BRPI0915949B1 (en) | 2020-09-15 |
US8346454B2 (en) | 2013-01-01 |
CA2730924A1 (en) | 2010-01-21 |
US8326506B2 (en) | 2012-12-04 |
WO2010009317A1 (en) | 2010-01-21 |
US20110320101A1 (en) | 2011-12-29 |
ES2524365T3 (en) | 2014-12-05 |
BRPI0915949B8 (en) | 2023-01-10 |
JP2011528303A (en) | 2011-11-17 |
US8083295B2 (en) | 2011-12-27 |
EP2318243A1 (en) | 2011-05-11 |
US9056673B2 (en) | 2015-06-16 |
CN102099230A (en) | 2011-06-15 |
US20140032076A1 (en) | 2014-01-30 |
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